Airbus A300-600F vs. Airbus H225 Super Puma

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Airbus A300-600F versus Airbus H225 Super Puma
54.08 m 177 ft 5 in length 14.06 m 46 ft 2 in
17.05 m 55 ft 11 in height 4.38 m 14 ft 4 in
44.84 m 147 ft 1 in wingspan
2 x General Electric CF6-80C2A5 turbofan engines engines 2 x Turbomeca Makila 2A turboshaft engines
Approximately 59,000 lbf per engine thrust per engine 2,778 hp
Approximately 118,000 lbf total total thrust 5,556 hp
170,000 kg 374,786 lb MTOW 11,000 kg 24,251 lb
4,830 km 2,608 nm range 857 km 463 nm
860 km/h 534 mph cruise speed 242 km/h 150 mph
capacity 24-28
rotor diameter 16.2 m 53 ft 2 in
rate of climb 10.7 m/s 2,106 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.